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High Thrust-Density Electrostaic Engines Project
<p>These issues are addressable by: increasing the thrust, power, and thrust-to-power ratio capability of EP systems; reducing the non-recurring engineering systems costs; and developing system architectures with performance characteristics that capture the broadest possible range of missions so that development & flight costs are amortized over multiple users. We believe these objectives can be achieved by developing the Next Generation Electric Propulsion Thruster (NGEPT); a GRC-patented modular EP device based on a new arrangement of relatively mature and proven technologies with the potential to yield revolutionary capabilities</p>
Complete Metadata
| @type | dcat:Dataset |
|---|---|
| accessLevel | public |
| bureauCode |
[
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|
| contactPoint |
{
"fn": "Michael Patterson",
"@type": "vcard:Contact",
"hasEmail": "mailto:michael.s.patterson@faa.gov"
}
|
| description | <p>These issues are addressable by: increasing the thrust, power, and thrust-to-power ratio capability of EP systems; reducing the non-recurring engineering systems costs; and developing system architectures with performance characteristics that capture the broadest possible range of missions so that development &amp; flight costs are amortized over multiple users.&nbsp; We believe these objectives can be achieved by developing the Next Generation Electric Propulsion Thruster (NGEPT); a GRC-patented modular EP device based on a new arrangement of relatively mature and proven technologies with the potential to yield revolutionary capabilities</p> |
| distribution |
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|
| identifier | TECHPORT_14697 |
| issued | 2014-04-01 |
| keyword |
[
"completed",
"glenn-research-center",
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|
| landingPage | http://techport.nasa.gov/view/14697 |
| modified | 2025-04-01 |
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|
| temporal | 2014-04-01T00:00:00Z/2014-09-01T00:00:00Z |
| title | High Thrust-Density Electrostaic Engines Project |